Loong M9 Chinese Unmanned Aerial Vehicle (UAV)
Loong M9
Tactical Unmanned Aerial Vehicle (UAV)
Other
Basic Information
Name
Loong M9 Chinese Unmanned Aerial Vehicle (UAV)
Designation
Loong M9
Alternate Designation
Loong M9
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Loong UAV
Date of Introduction
2025
Description
The Loong M9 Chinese Unmanned Aerial Vehicle (UAV) features a delta-wing airframe with a rear-mounted pusher propeller, mirroring the Shahed-136's architecture. The airframe is manufactured through carbon-fiber integrated molding, providing structural strength while minimizing weight. The drone incorporates mild rain resistance and an IP54 environmental protection rating to support operations across varied climates.
Air & Air Defense Specifications
Engine
The system uses a 550 cc EFI (Electronic Fuel Injection) piston engine with a starter generator capable of 1,000 W at 28 V, paired with a 33-inch propeller. This design choice emphasizes reliability and ease of maintenance compared to more complex turbocharged or turbine solutions
Max Speed
223.0 km/h
Cruise Speed
190.0 km/h
Range
1620.0 km
Endurance
8.00 hrs
Service Ceiling
4500 m
Wingspan
2.50 m
Payload Capacity
50 kg
System
Alternate Designation
Loong M9
Type
Unmanned Aerial Vehicle (UAV)
Manufacturer
Loong UAV
Payload Capacity
50 kg
Guidance & Navigation
The M9 integrates an advanced guidance suite designed for resilience in contested electromagnetic environments: Anti-GPS/No-GPS Operation: The drone can navigate and hover without GPS signals, relying on inertial measurement systems; GPS-Free Precision Landing: Enhanced accuracy without external positioning signals; Anti-Jamming Data Link: Frequency-hopping broadband communication and multi-band satellite positioning resist electronic interference; Multi-Array Navigation: Employs diverse positioning methods for redundancy.
Operating Temperature
−25°C to +60°C
Launch System
The M9 employs a rocket-assisted catapult system for rapid deployment. The rocket booster generates 20 kN of total impulse thrust at 20°C with a burn duration of 2.0±0.2 seconds, with a weight not exceeding 23 kg excluding the bracket.
Dimensions
Length
3.5 m
Height
INA
Wingspan
2.5 m
Maximum Takeoff Weight
200 kg
Automotive
Engine Name
INA
Engine Type
The system uses a 550 cc EFI (Electronic Fuel Injection) piston engine with a starter generator capable of 1,000 W at 28 V, paired with a 33-inch propeller. This design choice emphasizes reliability and ease of maintenance compared to more complex turbocharged or turbine solutions
Engine Power
INA
Fuel Tank Capacity
108 liters
Fuel Consumption
10–12 liters/hour
Maximum Speed
223 km/h
Cruise Speed
190 km/h
Maximum Range
1,620 km
Service Ceiling
4,500 m
Endurance
8-9 hours
Wind Resistance
Level 7 (50–61 km/h)
Armament
Note
Internal payload bay: Accommodates up to 50 kg of customizable warheads or mission equipment.
Details
Country of Origin
China
Category
UAVs
Air > UAVs
Filter Label
L
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
3.5 m
Width
2.5 m
Height
—
Weight
200 kg
Operators (1)
China
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